EP2807345A4 - Thrust balance system for gas turbine engine - Google Patents
Thrust balance system for gas turbine engineInfo
- Publication number
- EP2807345A4 EP2807345A4 EP13796982.0A EP13796982A EP2807345A4 EP 2807345 A4 EP2807345 A4 EP 2807345A4 EP 13796982 A EP13796982 A EP 13796982A EP 2807345 A4 EP2807345 A4 EP 2807345A4
- Authority
- EP
- European Patent Office
- Prior art keywords
- gas turbine
- turbine engine
- balance system
- thrust balance
- thrust
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/001—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between stator blade and rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/02—Preventing or minimising internal leakage of working-fluid, e.g. between stages by non-contact sealings, e.g. of labyrinth type
- F01D11/025—Seal clearance control; Floating assembly; Adaptation means to differential thermal dilatations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D3/00—Machines or engines with axial-thrust balancing effected by working-fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/44—Free-space packings
- F16J15/441—Free-space packings with floating ring
- F16J15/442—Free-space packings with floating ring segmented
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/38—Retaining components in desired mutual position by a spring, i.e. spring loaded or biased towards a certain position
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261591434P | 2012-01-27 | 2012-01-27 | |
US13/444,898 US20130195627A1 (en) | 2012-01-27 | 2012-04-12 | Thrust balance system for gas turbine engine |
PCT/US2013/021711 WO2013180762A1 (en) | 2012-01-27 | 2013-01-16 | Thrust balance system for gas turbine engine |
Publications (4)
Publication Number | Publication Date |
---|---|
EP2807345A1 EP2807345A1 (en) | 2014-12-03 |
EP2807345A4 true EP2807345A4 (en) | 2015-11-04 |
EP2807345B1 EP2807345B1 (en) | 2018-03-07 |
EP2807345B2 EP2807345B2 (en) | 2020-11-18 |
Family
ID=48870362
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP13796982.0A Active EP2807345B2 (en) | 2012-01-27 | 2013-01-16 | Thrust balance system for gas turbine engine |
Country Status (3)
Country | Link |
---|---|
US (1) | US20130195627A1 (en) |
EP (1) | EP2807345B2 (en) |
WO (1) | WO2013180762A1 (en) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3088702A1 (en) | 2011-12-30 | 2016-11-02 | United Technologies Corporation | Gas turbine engine gear train |
EP2961942B1 (en) | 2013-02-28 | 2020-07-08 | United Technologies Corporation | Method and apparatus for handling pre-diffuser airflow for cooling gas turbine components |
US8641366B1 (en) | 2013-03-07 | 2014-02-04 | United Technologies Corporation | Non-contacting seals for geared gas turbine engine bearing compartments |
US10443443B2 (en) | 2013-03-07 | 2019-10-15 | United Technologies Corporation | Non-contacting seals for geared gas turbine engine bearing compartments |
US10801348B2 (en) * | 2014-10-14 | 2020-10-13 | Raytheon Technologies Corporation | Non-contacting dynamic seal |
US20170051751A1 (en) * | 2015-08-19 | 2017-02-23 | United Technologies Corporation | Seal assembly for rotational equipment |
US10060280B2 (en) | 2015-10-15 | 2018-08-28 | United Technologies Corporation | Turbine cavity sealing assembly |
US20170107839A1 (en) * | 2015-10-19 | 2017-04-20 | United Technologies Corporation | Rotor seal and rotor thrust balance control |
US20170130732A1 (en) * | 2015-11-06 | 2017-05-11 | United Technologies Corporation | Compressor exit seal |
US10428672B2 (en) | 2016-02-08 | 2019-10-01 | United Technologies Corporation | Floating, non-contact seal and dimensions thereof |
US10060535B2 (en) * | 2016-02-25 | 2018-08-28 | United Technologies Corporation | Shaped spring element for a non-contact seal device |
US10344614B2 (en) | 2016-04-12 | 2019-07-09 | United Technologies Corporation | Active clearance control for a turbine and case |
US11053797B2 (en) * | 2017-01-23 | 2021-07-06 | General Electric Company | Rotor thrust balanced turbine engine |
US10731761B2 (en) | 2017-07-14 | 2020-08-04 | Raytheon Technologies Corporation | Hydrostatic non-contact seal with offset outer ring |
WO2019168501A1 (en) * | 2018-02-27 | 2019-09-06 | Siemens Aktiengesellschaft | Turbine cooling air delivery system |
GB201807840D0 (en) * | 2018-05-15 | 2018-06-27 | Rolls Royce Plc | Gas turbine engine |
US11421543B2 (en) * | 2018-11-28 | 2022-08-23 | Raytheon Technologies Corporation | Hydrostatic seal with asymmetric beams for anti-tipping |
US11199102B2 (en) | 2018-11-28 | 2021-12-14 | Raytheon Technologies Corporation | Hydrostatic seal with increased design space |
US11674402B2 (en) | 2018-11-28 | 2023-06-13 | Raytheon Technologies Corporation | Hydrostatic seal with non-parallel beams for anti-tipping |
US11111805B2 (en) | 2018-11-28 | 2021-09-07 | Raytheon Technologies Corporation | Multi-component assembled hydrostatic seal |
US11203934B2 (en) | 2019-07-30 | 2021-12-21 | General Electric Company | Gas turbine engine with separable shaft and seal assembly |
US11473439B1 (en) | 2021-09-23 | 2022-10-18 | General Electric Company | Gas turbine engine with hollow rotor in fluid communication with a balance piston cavity |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5284347A (en) * | 1991-03-25 | 1994-02-08 | General Electric Company | Gas bearing sealing means |
US20070007730A1 (en) * | 2004-05-28 | 2007-01-11 | Garrison Glenn M | Air riding seal |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2647684A (en) | 1947-03-13 | 1953-08-04 | Rolls Royce | Gas turbine engine |
US3121526A (en) * | 1960-08-25 | 1964-02-18 | Rolls Royce | Gas turbine engines |
US3433020A (en) † | 1966-09-26 | 1969-03-18 | Gen Electric | Gas turbine engine rotors |
US4251987A (en) | 1979-08-22 | 1981-02-24 | General Electric Company | Differential geared engine |
US4653267A (en) | 1983-05-31 | 1987-03-31 | United Technologies Corporation | Thrust balancing and cooling system |
GB2234035B (en) * | 1989-07-21 | 1993-05-12 | Rolls Royce Plc | A reduction gear assembly and a gas turbine engine |
US5760289A (en) | 1996-01-02 | 1998-06-02 | General Electric Company | System for balancing loads on a thrust bearing of a gas turbine engine rotor and process for calibrating control therefor |
JP3537349B2 (en) * | 1998-04-20 | 2004-06-14 | 日機装株式会社 | Thrust balance device |
US8172232B2 (en) † | 2003-05-01 | 2012-05-08 | Advanced Technologies Group, Inc. | Non-contact seal for a gas turbine engine |
US8002285B2 (en) * | 2003-05-01 | 2011-08-23 | Justak John F | Non-contact seal for a gas turbine engine |
GB0412476D0 (en) | 2004-06-04 | 2004-07-07 | Rolls Royce Plc | Seal system |
US8092150B2 (en) * | 2007-07-04 | 2012-01-10 | Alstom Technology Ltd. | Gas turbine with axial thrust balance |
US8381533B2 (en) † | 2009-04-30 | 2013-02-26 | Honeywell International Inc. | Direct transfer axial tangential onboard injector system (TOBI) with self-supporting seal plate |
US8176725B2 (en) † | 2009-09-09 | 2012-05-15 | United Technologies Corporation | Reversed-flow core for a turbofan with a fan drive gear system |
US10119476B2 (en) † | 2011-09-16 | 2018-11-06 | United Technologies Corporation | Thrust bearing system with inverted non-contacting dynamic seals for gas turbine engine |
-
2012
- 2012-04-12 US US13/444,898 patent/US20130195627A1/en not_active Abandoned
-
2013
- 2013-01-16 WO PCT/US2013/021711 patent/WO2013180762A1/en active Application Filing
- 2013-01-16 EP EP13796982.0A patent/EP2807345B2/en active Active
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5284347A (en) * | 1991-03-25 | 1994-02-08 | General Electric Company | Gas bearing sealing means |
US20070007730A1 (en) * | 2004-05-28 | 2007-01-11 | Garrison Glenn M | Air riding seal |
Non-Patent Citations (1)
Title |
---|
See also references of WO2013180762A1 * |
Also Published As
Publication number | Publication date |
---|---|
EP2807345B2 (en) | 2020-11-18 |
EP2807345A1 (en) | 2014-12-03 |
WO2013180762A1 (en) | 2013-12-05 |
EP2807345B1 (en) | 2018-03-07 |
US20130195627A1 (en) | 2013-08-01 |
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